SHUTTLE TRAJECTORY DATA
Lift off time (UTC) : 2006/252/15:14:54 972 Area (sq ft) : 1208 48 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 76 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 16339
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
262/15:29:52
459 -0
5 0
0 0
8
010/00:14:57
487 0
3 0
8 190
6
000/00:00:02
974 -0
5 0
0 179
5
Coasting Arc #1 (Orbit 142)
---------------------------------------
Vector Time (GMT): 2006/261/13:45:12
000
Vector Time (MET): 008/22:30:17
028
Weight (LBS) : 209762
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1584807
42 A = 6719057
27 meter
Y = 4836675
61 meter E =
0012303
Z = 4373997
64 I = 51
91168
XDOT = -5050
512389 Wp = 44
48880
YDOT = -4730
248244 meter/sec RA = 65
79980 deg
ZDOT = 3403
562415 TA = 11
41588
MA = 11
38800
Ha = 190
475 n
mi
Hp = 179
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5199499
42 X = -1660079
31
Y = 15868358
30 feet Y = 4818513
21 meter
Z = 14350385
95 Z = 4366115
89
XDOT = -16569
922537 XDOT = -5013
719447
YDOT = -15519
187151 feet/sec YDOT = -4786
580108 meter/sec
ZDOT = 11166
543357 ZDOT = 3379
116620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1316026
47 X = -401124
87
Y = -16671252
61 feet Y = -5081397
79 meter
Z = 14321682
06 Z = 4365248
69
XDOT = 20145
518835 XDOT = 6140
354141
YDOT = 7915
578035 feet/sec YDOT = 2412
668185 meter/sec
ZDOT = 11074
825121 ZDOT = 3375
606697
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 29391U 06036A 06261
62662785
00014500 00000-0 95600-4 0 9002
2 29391 51
6316 66
1235 0011996 359
1322
9819 15
75684271 1433
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06261
62662785 = yrday
fracday
Element set: 900
Inclination: 51
6316 deg
RA of node: 66
1235 deg
Eccentricity:
0011996
Arg of perigee: 359
1322 deg
Mean anomaly:
9819 deg
Mean motion: 15
75684271 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 143
Checksum: 303
Coasting Arc #2 (Orbit 157)
---------------------------------------
Vector Time (GMT): 2006/262/13:50:10
700
Vector Time (MET): 009/22:35:15
728
Weight (LBS) : 209762
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3787864
92 A = 6727202
78 meter
Y = 5489429
31 meter E =
0021528
Z = -775872
17 I = 51
92693
XDOT = -3548
416570 Wp = 19
83961
YDOT = 3287
838844 meter/sec RA = 60
62169 deg
ZDOT = 6006
341118 TA = 331
71973
MA = 331
83645
Ha = 190
653 n
mi
Hp = 179
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12427378
35 X = 3729902
96
Y = 18009938
67 feet Y = 5531508
00 meter
Z = -2545512
36 Z = -757611
75
XDOT = -11641
786646 XDOT = -3614
134106
YDOT = 10786
872849 feet/sec YDOT = 3247
748486 meter/sec
ZDOT = 19705
843563 ZDOT = 5988
943353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18915219
14 X = -5765358
79
Y = -11016239
71 feet Y = -3357749
86 meter
Z = -2476732
63 Z = -754908
10
XDOT = 5249
610562 XDOT = 1600
081299
YDOT = -13378
138645 feet/sec YDOT = -4077
656659 meter/sec
ZDOT = 19641
476253 ZDOT = 5986
721962
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 29391U 06036A 06262
57796498
00014500 00000-0 95600-4 0 9017
2 29391 51
6326 61
2253 0012122 3
2381 356
8859 15
75663476 1581
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
57796498 = yrday
fracday
Element set: 901
Inclination: 51
6326 deg
RA of node: 61
2253 deg
Eccentricity:
0012122
Arg of perigee: 3
2381 deg
Mean anomaly: 356
8859 deg
Mean motion: 15
75663476 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 158
Checksum: 316
Coasting Arc #3 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2006/262/15:29:53
946
Vector Time (MET): 010/00:14:58
974
Weight (LBS) : 209742
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1517606
47 A = 6725258
31 meter
Y = 6152811
60 meter E =
0021702
Z = 2209013
98 I = 51
91926
XDOT = -5353
895719 Wp = 40
07376
YDOT = -664
207160 meter/sec RA = 60
29374 deg
ZDOT = 5514
748610 TA = 344
64494
MA = 344
71069
Ha = 190
605 n
mi
Hp = 179
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4979023
84 X = 1437887
67
Y = 20186389
78 feet Y = 6169354
24 meter
Z = 7247421
19 Z = 2216192
69
XDOT = -17565
274667 XDOT = -5372
851376
YDOT = -2179
157348 feet/sec YDOT = -724
247163 meter/sec
ZDOT = 18093
007251 ZDOT = 5488
693550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18661574
14 X = -5688047
80
Y = -9144728
58 feet Y = -2787313
27 meter
Z = 7275006
15 Z = 2217421
87
XDOT = 12326
544476 XDOT = 3757
130756
YDOT = -10803
298094 feet/sec YDOT = -3292
845259 meter/sec
ZDOT = 17995
847051 ZDOT = 5485
134181
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 29391U 06036A 06262
70480845
00014500 00000-0 95600-4 0 9029
2 29391 51
6322 60
5722 0012124 3
5875 356
5374 15
75681180 1607
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06262
70480845 = yrday
fracday
Element set: 902
Inclination: 51
6322 deg
RA of node: 60
5722 deg
Eccentricity:
0012124
Arg of perigee: 3
5875 deg
Mean anomaly: 356
5374 deg
Mean motion: 15
75681180 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 160
Checksum: 284
Coasting Arc #4 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2006/263/15:30:06
751
Vector Time (MET): 011/00:15:11
779
Weight (LBS) : 209742
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4915669
40 A = 6718583
69 meter
Y = 878632
62 meter E =
0013669
Z = -4499241
33 I = 51
88190
XDOT = 1690
064816 Wp = 50
48964
YDOT = 6800
539305 meter/sec RA = 55
12047 deg
ZDOT = 3189
419931 TA = 251
20893
MA = 251
35726
Ha = 190
741 n
mi
Hp = 179
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16127524
27 X = 4927324
35
Y = 2882652
94 feet Y = 933726
00 meter
Z = -14761290
45 Z = -4475332
83
XDOT = 5544
832073 XDOT = 1598
319832
YDOT = 22311
480658 feet/sec YDOT = 6818
945277 meter/sec
ZDOT = 10463
976151 ZDOT = 3197
407141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12406062
47 X = -3781367
84
Y = 10822271
19 feet Y = 3298628
26 meter
Z = -14672098
80 Z = -4472055
72
XDOT = -20034
476087 XDOT = -6106
508311
YDOT = -8805
117434 feet/sec YDOT = -2683
799794 meter/sec
ZDOT = 10494
661823 ZDOT = 3198
772924
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 29391U 06036A 06263
65613530
00014500 00000-0 95600-4 0 9034
2 29391 51
6323 55
6745 0012167 6
8668 353
2661 15
75714693 1756
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06263
65613530 = yrday
fracday
Element set: 903
Inclination: 51
6323 deg
RA of node: 55
6745 deg
Eccentricity:
0012167
Arg of perigee: 6
8668 deg
Mean anomaly: 353
2661 deg
Mean motion: 15
75714693 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 175
Checksum: 308
Coasting Arc #5 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2006/264/15:35:09
676
Vector Time (MET): 012/00:20:14
705
Weight (LBS) : 209742
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 416215
89 A = 6718547
92 meter
Y = -4993677
67 meter E =
0019178
Z = -4493268
88 I = 51
86462
XDOT = 6116
713818 Wp = 36
08293
YDOT = 3391
332341 meter/sec RA = 50
01703 deg
ZDOT = -3194
135866 TA = 201
99461
MA = 202
07702
Ha = 190
776 n
mi
Hp = 179
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1365537
71 X = 493911
89
Y = -16383456
92 feet Y = -4988583
68 meter
Z = -14741695
80 Z = -4491057
95
XDOT = 20067
958722 XDOT = 6093
812189
YDOT = 11126
418442 feet/sec YDOT = 3459
677370 meter/sec
ZDOT = -10479
448379 ZDOT = -3164
476642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12296960
86 X = 3748113
67
Y = 10921986
93 feet Y = 3329021
62 meter
Z = -14734140
77 Z = -4490966
11
XDOT = -20129
496238 XDOT = -6135
470453
YDOT = 8639
454274 feet/sec YDOT = 2633
305663 meter/sec
ZDOT = -10368
491814 ZDOT = -3160
316305
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
SHUTTLE
1 29391U 06036A 06264
67086453
00014500 00000-0 95600-4 0 9046
2 29391 51
6324 50
4490 0012196 10
2921 349
8490 15
75714138 1913
Satellite: SHUTTLE
Catalog Number: 29391
Epoch time: 06264
67086453 = yrday
fracday
Element set: 904
Inclination: 51
6324 deg
RA of node: 50
4490 deg
Eccentricity:
0012196
Arg of perigee: 10
2921 deg
Mean anomaly: 349
8490 deg
Mean motion: 15
75714138 rev/day
Decay rate: 1
45000E-04 rev/day^2
Epoch rev: 191
Checksum: 297
SPACE SHUTTLE ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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